[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

WO2008037941A1 - A method of producing substoichiometric oxides of titanium by reduction with hydrogen - Google Patents

A method of producing substoichiometric oxides of titanium by reduction with hydrogen Download PDF

Info

Publication number
WO2008037941A1
WO2008037941A1 PCT/GB2006/003573 GB2006003573W WO2008037941A1 WO 2008037941 A1 WO2008037941 A1 WO 2008037941A1 GB 2006003573 W GB2006003573 W GB 2006003573W WO 2008037941 A1 WO2008037941 A1 WO 2008037941A1
Authority
WO
WIPO (PCT)
Prior art keywords
interior space
precursor
heating
kiln
titanium
Prior art date
Application number
PCT/GB2006/003573
Other languages
French (fr)
Inventor
Alexander Simpson
Philip Carter
Original Assignee
Atranova Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Atranova Limited filed Critical Atranova Limited
Priority to US12/443,091 priority Critical patent/US20100040533A1/en
Priority to JP2009529748A priority patent/JP2010504903A/en
Priority to CN200680056210A priority patent/CN101547863A/en
Priority to AU2006348872A priority patent/AU2006348872A1/en
Priority to CA002664733A priority patent/CA2664733A1/en
Priority to EP06794576A priority patent/EP2066587A1/en
Priority to PCT/GB2006/003573 priority patent/WO2008037941A1/en
Publication of WO2008037941A1 publication Critical patent/WO2008037941A1/en
Priority to IL197840A priority patent/IL197840A0/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J6/00Heat treatments such as Calcining; Fusing ; Pyrolysis
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01GCOMPOUNDS CONTAINING METALS NOT COVERED BY SUBCLASSES C01D OR C01F
    • C01G23/00Compounds of titanium
    • C01G23/04Oxides; Hydroxides
    • C01G23/043Titanium sub-oxides
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/46Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on titanium oxides or titanates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS, OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B5/00Muffle furnaces; Retort furnaces; Other furnaces in which the charge is held completely isolated
    • F27B5/04Muffle furnaces; Retort furnaces; Other furnaces in which the charge is held completely isolated adapted for treating the charge in vacuum or special atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D5/00Supports, screens, or the like for the charge within the furnace
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J2219/00Chemical, physical or physico-chemical processes in general; Their relevant apparatus
    • B01J2219/00049Controlling or regulating processes
    • B01J2219/00051Controlling the temperature
    • B01J2219/00132Controlling the temperature using electric heating or cooling elements
    • B01J2219/00135Electric resistance heaters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01JCHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
    • B01J2219/00Chemical, physical or physico-chemical processes in general; Their relevant apparatus
    • B01J2219/00049Controlling or regulating processes
    • B01J2219/00051Controlling the temperature
    • B01J2219/0015Controlling the temperature by thermal insulation means
    • B01J2219/00155Controlling the temperature by thermal insulation means using insulating materials or refractories
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01PINDEXING SCHEME RELATING TO STRUCTURAL AND PHYSICAL ASPECTS OF SOLID INORGANIC COMPOUNDS
    • C01P2004/00Particle morphology
    • C01P2004/60Particles characterised by their size
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/652Reduction treatment
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • C04B2235/6562Heating rate
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
    • C04B2235/6567Treatment time
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658Atmosphere during thermal treatment
    • C04B2235/6582Hydrogen containing atmosphere
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658Atmosphere during thermal treatment
    • C04B2235/6586Processes characterised by the flow of gas
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/79Non-stoichiometric products, e.g. perovskites (ABO3) with an A/B-ratio other than 1
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/96Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
    • C04B2235/9646Optical properties
    • C04B2235/9661Colour

Definitions

  • the present invention relates to a method for the production of substoichiometric oxides of titanium known as Magneli phases, and in particular those commercially produced and commonly referred to as Ebonex®.
  • Magneli phases are members of the series of substoichiometric oxides of titanium with the general formula Ti n O 2n - I where the number n is between 4 and 10. Each phase is separate and identifiable, with a distinct structural identity. Magneli phases exhibit desirable electrochemical properties. In particular, they possess a high electrical conductivity, comparable to that of graphite, while also, being ceramic materials, they are exceedingly resistant to corrosion.
  • Magneli phases The most highly conductive of the Magneli phases is the lowest Magneli phase Ti 4 O 7 , followed by Ti 5 O 9 .
  • Materials made from the more conductive Magneli phases with the amounts OfTi 4 O 7 and Ti 5 O 9 maximised in order to obtain high conductivity combined with high corrosion resistance have been manufactured commercially under the name 'Ebonex®'. This has been produced in many different forms, including plates, rods, tubes and powder.
  • Magneli phases are produced by high temperature reduction of titanium oxides in a hydrogen atmosphere.
  • the conductivity of the resulting material depends upon the particular Magneli phase(s) produced.
  • Ebonex® articles in the following manner: 1) Articles of TiO 2 starting material were placed horizontally in ceramic saggers layered with powdered activated carbon.
  • the applicant has found that the above process is inconsistent in its production of Ebonex® material and often requires repeated "cooking" of the article which results in high losses due to breakages. There are also issues with operational failure of the Ebonex® as a consequence of not forming the correct balance of the desired Magneli phases.
  • the Ebonex® material formed would consist entirely of Ti 4 O 7 , the most conductive of the Magneli phases. In practice, however, some Ti 3 O 5 is invariably formed also.
  • a readily achievable balance of phases is for no more than 4% Ti 3 O 5 with at least 30% Ti 4 O 7 and/or at least 50% Ti 4 O 7 and Ti 5 O 9 , the remainder being made up of the other higher oxides.
  • the present invention therefore aims to provide an alternative process for manufacturing Magneli phases, and Ebonex® in particular, that overcomes, or at least alleviates, one or more of the problems discussed above.
  • the present invention provides a method of manufacturing substoichiometric oxides of titanium (such as Ebonex®), the method comprising: holding a titanium oxide precursor into the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space in order to heat the precursor and the reducing gas, to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium.
  • the method is such that the precursor is held in the interior space so that said reducing gas can substantially fully envelop the precursor.
  • the method preferably uses convection as the main method of heating the precursor.
  • a thermal shield is preferably used to minimise or at least reduce heating caused by radiant heat produced by the heating elements.
  • the inventors have found that reducing radiant heating of the precursor reduces cracking and over reduction.
  • a ceramic fibre blanket is preferably used as the thermal shield between the precursor and the heating elements.
  • a gap is preferably provided between the thermal insulator and a support used to hold the precursor.
  • a support is provided by means of four box- like frames, each being able to hold 96 precursor rods within the interior space of the kiln, thus allowing a total of 384 rods to be produced during each heating and reduction cycle.
  • the heating of the interior space is preferably controlled so that during an initial heating stage the interior space is heated at a rate not exceeding about 200 0 C per hour, until the interior space reaches a predetermined operating temperature above 1170 0 C.
  • the temperature of the interior ⁇ pace is maintained within a temperature range between 1170 0 C and 1190 0 C for a period of time of between five and eight hours.
  • the introduction of the reducing gas is controlled so that the reducing gas is introduced at a predetermined rate during said heating step.
  • the reducing gas is introduced at a rate of between two and five cubic meters per hour.
  • the precursor can be held by or suspended from the support. Suspension of the precursor is preferred as this is easy to achieve for monolithic precursors having various different shapes (such as rods, tubes, plates, tiles etc).
  • a desiccant such as powdered activated carbon
  • a desiccant helps to absorb moisture that is generated and thereby helps to reduce cracks in the resulting precursor.
  • the resulting precursor can be pulverised to form powdered substoichiometric oxides of titanium.
  • Figure 1 is a three dimensional part cut away view of a kiln used in a novel process for the manufacture of Ebonex® rods;
  • Figure 2 is a cross-sectional view of the kiln shown in Figure 1;
  • Figure 3 is a flow chart showing the steps taken to make the Ebonex® rods using the kiln shown in Figure 1;
  • Figure 4 is a plot showing the way in which the temperature of the kiln is varied during the manufacturing process.
  • Kiln Figure 1 is a part cut-away view of a kiln assembly 1 used to make Ebonex® rods and Figure 2 is a cross-sectional view of the kiln assembly 1.
  • the kiln assembly 1 includes a heat resistant hood 3 which defines an interior space 5 above a brick base 6. Heating elements 7 are provided on the inside and adjacent the hood 3 for heating the interior space 5.
  • the interior space 5 is sealed by positioning the hood 3 in an oil filled trough 8 that surrounds the brick base 6.
  • the top of the kiln 1 has a gas inlet 10 and a vent 14.
  • a gas outlet 12 is provided through the base 6.
  • the frames 9 are provided for suspending precursor rods (tubes) 11, made of titanium oxide, within the interior space 5 of the kiln 1.
  • the frames 9 are made from a high-temperature alloy, such as Inconel® nickel-chromium-iron 601 alloy.
  • each frame 9 includes a top plate 13 having 96 circular holes 15 arranged in a regular array (ie arranged in rows and columns), through which the precursor rods 11 are suspended.
  • the inventors found that these holes 15 should be sized to have a diameter that is greater than 1.2 times the diameter of the precursor rods 11 in order to provide room for the expansion of the rods 11 during the heating and reduction process. The inventors found that when smaller holes are used more of the rods 11 cracked during the heating and reduction process.
  • the holes 15 are sized in the above manner so that they can be used with rods 11 having a diameter of up to 18mm.
  • each precursor rod 11 is suspended under its own weight from the top plate 13 by a pin 17, which is inserted through a hole 19 at the top of the rod 11 (which passes through the rod 11 in a direction perpendicular to the rod's longitudinal axis).
  • the pins 17 are preferably aligned with each other in order to reduce the likelihood of the rods 11 swinging into each other during the heating and reduction process.
  • the rods 11 are approximately 200mm long and each frame 9 is dimensioned so that each rod 11 hangs freely within the interior space 5 above a tray 21 filled with powdered activated carbon 23. In this way, during the heating and reduction process, the hydrogen gas used for the reduction can substantially fully envelop the rods 11.
  • the carbon 23 is provided (in powdered, solid or granular form) for removing excess moisture from the interior space 5 during the heating and reduction process.
  • the inventors have found that without the carbon 23, there is a greater risk of over reduction which affects the formation of the desired Magneli phases. Over time, the absorption of water vapour results in the carbon 23 being consumed as it is converted into carbon dioxide.
  • the activated carbon 23 must, therefore, be replenished or replaced from time to time. In the preferred embodiment, the carbon is replaced every three production cycles.
  • the four frames 9 are positioned side by side in two rows and two columns and the outer sides of the frames 9 (ie the sides closest to the heating elements 7) are clad in a protective shielding 25, such as a ceramic fibre or a low thermal mass insulation blanket, to minimise (if not avoid) the exposure of the rods 11 to direct radiant heat from the heating elements 7.
  • the protective shielding 25 is standard grade Fiberfrax® Durablanket® of 96 kg/m 3 density and 25 mm thick, which is made of blown alumino-silicate ceramic fibre and classified to operate at temperatures of 125O 0 C.
  • the shielding 25 is attached to the frames 9 and hangs down below the bottom of the rods 11.
  • a gap 26 of approximately 25mm is provided between the bottom of the shielding 25 and the tray 21 to allow for good circulation of the hydrogen gas during the heating and reduction process.
  • An oxygen meter (not shown) and two thermocouples (not shown) are located at different positions in the interior space 5 and are provided for generating measurements to aid in the control of the manufacturing process.
  • Production Process Figure 3 is a flowchart illustrating the production process used in this embodiment.
  • the kiln assembly 1 is prepared, by suspending the rods 11 of titanium oxide from the frames 9; adding activated carbon 23; sealing the internal space 5 by lowering the hood 3 into the oil-filled trough 8; opening the inlet 10 and the outlet 12 and closing the top vent 14.
  • nitrogen is pumped into the inlet 10, in step S3, at a rate of approximately three cubic meters per hour for a minimum of fifty minutes, in order to purge the interior space 5 of oxygen.
  • An oxygen meter (not shown) is used to confirm when the oxygen has been removed to the 2% level.
  • step S5 hydrogen is pumped into the inlet 10 at a rate of approximately four cubic meters per hour. Hydrogen will continue to be pumped into the inlet 10 until the end of the heating and reduction process and throughout the subsequent cooling.
  • the oxygen meter is again consulted to ensure the remaining oxygen level is below 2% before a further oxygen test is undertaken. This test includes filling a small container with gas from the outlet 12 and, at a safe distance, applying a lit taper to the container. If the gas held within the container ignites with a loud pop, then this indicates that the oxygen level in the interior space 5 remains too high to proceed with the reduction process. Whereas, if the gas held within the container burns slowly, with a lazy flame, then it is safe to proceed with the reduction process. The hydrogen escaping at the outlet 12 is then lit and allowed to burn off as the reduction process proceeds.
  • the heating process is then started, in step S7, by switching on the heating elements 7.
  • the initial heating is controlled in steps S9 and Sl 1 by a controller so that the interior space 5 is heated at a rate not exceeding 200 0 C /hour.
  • the controller maintains the operating temperature in step S15 for approximately 5.5 hours.
  • the heating elements 7 are switched off and the kiln 1 is allowed to cool naturally in step S 16 until the internal temperature is below 200 0 C (which typically takes about fourteen hours).
  • Figure 4 shows the typical temperature variation inside the kiln 1 during the production process and illustrating the initial heating stage, the reduction stage and the cooling stage.
  • step S 17 the hydrogen flow is halted, the outlet 12 is closed and the top vent 14 is opened. Nitrogen gas is then pumped in via the inlet 10 into the internal space 5 to purge the hydrogen gas out via the top vent 14 where it is lit and allowed to burn off. Once the flame has extinguished, indicating that there is no more hydrogen within the interior space 5, the hood 3 is removed in step S19 and the rods 11 are removed and tested in step S20. In this embodiment in step S20, each rod 11 is tested using the following semi- empirical tests:
  • a two-point probe electrical conductivity test in which a current of 100 mA is passed through the rod 11 and the voltage drop measured between two probes on the rod 11 that are a placed 100 mm apart from each other is compared with a threshold and if it is greater then the rod fails.
  • X-ray diffraction measurements may be obtained on some or all of the rods 11 to confirm the Magneli phases that are present.
  • the average voltage drop is about 35 millivolts.
  • similar tests performed on rods manufactured using the prior art technique results in typical measured voltage drops in the range of 65 to 70 millivolts, with some as high as 120 to 130 millivolts. In the latter case, those rods would then be reprocessed by running them through the heating and reduction process again.
  • the precursor rods were hung from a frame within the kiln.
  • the rods may be stood directly on the floor of the kiln 1, but the inventors found that this resulted in a greater percentage of the rods being broken during the heating and reduction process, hi a further alternative, the precursors may be supported by one or more supports so that they can be fully enveloped by the reducing gas.
  • precursor tubular rods were heated in the kiln to produce Ebonex® tubular rods.
  • the precursors can be plates, tiles, sheets etc.
  • the resulting Ebonex® material may be pulverised to produce Ebonex® powder.
  • a controller was used to control the heating and reduction process.
  • this controller can be a human controller or an automated one.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Inorganic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

A method and apparatus are described for manufacturing Ebonex® articles such as rods and tiles from titanium oxide precursors. The precursors are held within the interior space of a kiln and heated in a reducing gas. The precursors are held so that the reducing gas is able to fully envelop them. In a preferred embodiment, the precursors are hung from a support within the kiln. The temperature of the kiln is also controlled to limit the initial heating of the kiln and to maintain the kiln within a predetermined range of operating temperatures.

Description

A METHOD OF PRODUCING SUBSTOICHIOMETRIC OXIDES OF TITANIUM BY REDUCTION WITH HYDROGEN
The present invention relates to a method for the production of substoichiometric oxides of titanium known as Magneli phases, and in particular those commercially produced and commonly referred to as Ebonex®.
Magneli phases are members of the series of substoichiometric oxides of titanium with the general formula TinO2n-I where the number n is between 4 and 10. Each phase is separate and identifiable, with a distinct structural identity. Magneli phases exhibit desirable electrochemical properties. In particular, they possess a high electrical conductivity, comparable to that of graphite, while also, being ceramic materials, they are exceedingly resistant to corrosion.
The most highly conductive of the Magneli phases is the lowest Magneli phase Ti4O7, followed by Ti5O9. Materials made from the more conductive Magneli phases with the amounts OfTi4O7 and Ti5O9 maximised in order to obtain high conductivity combined with high corrosion resistance have been manufactured commercially under the name 'Ebonex®'. This has been produced in many different forms, including plates, rods, tubes and powder.
There has been great interest in using these Magneli phases and Ebonex® in particular: as a ceramic electrode material in applications requiring the use of aggressive electrolytes; as a replacement for precious metal coated anodes; as electrodes for batteries and fuel cells; for electrowinning; for use in cathodic protection; electrochemical soil remediation; for the oxidation of organic wastes; and for water purification.
Magneli phases are produced by high temperature reduction of titanium oxides in a hydrogen atmosphere. The conductivity of the resulting material depends upon the particular Magneli phase(s) produced.
Previously, the applicant has manufactured Ebonex® articles in the following manner: 1) Articles of TiO2 starting material were placed horizontally in ceramic saggers layered with powdered activated carbon.
2) The saggers were then placed in a Bell furnace (kiln), where the temperature was raised to and held at 1180 0C for 8 hours, during which time the TiO2 material was left to undergo a reduction reaction in a hydrogen atmosphere. The rate of hydrogen addition was not usually controlled.
3) After 8 hours, the furnace was allowed to cool naturally until the temperature was at or below 200 0C, at which point the furnace was opened and the saggers removed from the furnace. 4) Each article was then visually inspected for cracks.
5) The presence of the desired Magneli phases in each article was then determined using a semi-empirical testing procedure.
The applicant has found that the above process is inconsistent in its production of Ebonex® material and often requires repeated "cooking" of the article which results in high losses due to breakages. There are also issues with operational failure of the Ebonex® as a consequence of not forming the correct balance of the desired Magneli phases. Ideally, the Ebonex® material formed would consist entirely of Ti4O7, the most conductive of the Magneli phases. In practice, however, some Ti3O5 is invariably formed also. A readily achievable balance of phases is for no more than 4% Ti3O5 with at least 30% Ti4O7 and/or at least 50% Ti4O7 and Ti5O9, the remainder being made up of the other higher oxides.
The present invention therefore aims to provide an alternative process for manufacturing Magneli phases, and Ebonex® in particular, that overcomes, or at least alleviates, one or more of the problems discussed above.
According to one aspect, the present invention provides a method of manufacturing substoichiometric oxides of titanium (such as Ebonex®), the method comprising: holding a titanium oxide precursor into the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space in order to heat the precursor and the reducing gas, to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium. The method is such that the precursor is held in the interior space so that said reducing gas can substantially fully envelop the precursor.
The method preferably uses convection as the main method of heating the precursor. When the heating is achieved using heating elements provided on the inside of the kiln, a thermal shield is preferably used to minimise or at least reduce heating caused by radiant heat produced by the heating elements. The inventors have found that reducing radiant heating of the precursor reduces cracking and over reduction. A ceramic fibre blanket is preferably used as the thermal shield between the precursor and the heating elements.
In order to facilitate the free circulation of the reducing gas around the precursor, a gap is preferably provided between the thermal insulator and a support used to hold the precursor.
In the embodiment to be described below, a support is provided by means of four box- like frames, each being able to hold 96 precursor rods within the interior space of the kiln, thus allowing a total of 384 rods to be produced during each heating and reduction cycle.
The heating of the interior space is preferably controlled so that during an initial heating stage the interior space is heated at a rate not exceeding about 200 0C per hour, until the interior space reaches a predetermined operating temperature above 1170 0C. In one embodiment the temperature of the interior ^pace is maintained within a temperature range between 1170 0C and 1190 0C for a period of time of between five and eight hours.
During the heating step, the introduction of the reducing gas is controlled so that the reducing gas is introduced at a predetermined rate during said heating step. In one embodiment the reducing gas is introduced at a rate of between two and five cubic meters per hour. The precursor can be held by or suspended from the support. Suspension of the precursor is preferred as this is easy to achieve for monolithic precursors having various different shapes (such as rods, tubes, plates, tiles etc).
The inventors have found, contrary to recent suggestions made by other Ebonex® manufacturers, that a desiccant (such as powdered activated carbon) provided in the interior space of the kiln during the heating and reduction process helps to absorb moisture that is generated and thereby helps to reduce cracks in the resulting precursor.
If desired, the resulting precursor can be pulverised to form powdered substoichiometric oxides of titanium.
These and other aspects of the present invention will become apparent from the following exemplary embodiments that are described with reference to the accompanying Figures in which:
Figure 1 is a three dimensional part cut away view of a kiln used in a novel process for the manufacture of Ebonex® rods;
Figure 2 is a cross-sectional view of the kiln shown in Figure 1;
Figure 3 is a flow chart showing the steps taken to make the Ebonex® rods using the kiln shown in Figure 1; and
Figure 4 is a plot showing the way in which the temperature of the kiln is varied during the manufacturing process.
Kiln Figure 1 is a part cut-away view of a kiln assembly 1 used to make Ebonex® rods and Figure 2 is a cross-sectional view of the kiln assembly 1. As shown in these Figures, the kiln assembly 1 includes a heat resistant hood 3 which defines an interior space 5 above a brick base 6. Heating elements 7 are provided on the inside and adjacent the hood 3 for heating the interior space 5. The interior space 5 is sealed by positioning the hood 3 in an oil filled trough 8 that surrounds the brick base 6. The top of the kiln 1 has a gas inlet 10 and a vent 14. A gas outlet 12 is provided through the base 6.
In this embodiment, four box-like frames 9 are provided for suspending precursor rods (tubes) 11, made of titanium oxide, within the interior space 5 of the kiln 1. In order to withstand the temperatures involved in the manufacturing process (to be described below), the frames 9 are made from a high-temperature alloy, such as Inconel® nickel-chromium-iron 601 alloy.
In this embodiment, each frame 9 includes a top plate 13 having 96 circular holes 15 arranged in a regular array (ie arranged in rows and columns), through which the precursor rods 11 are suspended. The inventors found that these holes 15 should be sized to have a diameter that is greater than 1.2 times the diameter of the precursor rods 11 in order to provide room for the expansion of the rods 11 during the heating and reduction process. The inventors found that when smaller holes are used more of the rods 11 cracked during the heating and reduction process. In this embodiment the holes 15 are sized in the above manner so that they can be used with rods 11 having a diameter of up to 18mm.
As shown in Figures 1 and 2, each precursor rod 11 is suspended under its own weight from the top plate 13 by a pin 17, which is inserted through a hole 19 at the top of the rod 11 (which passes through the rod 11 in a direction perpendicular to the rod's longitudinal axis). The pins 17 are preferably aligned with each other in order to reduce the likelihood of the rods 11 swinging into each other during the heating and reduction process. In this embodiment, the rods 11 are approximately 200mm long and each frame 9 is dimensioned so that each rod 11 hangs freely within the interior space 5 above a tray 21 filled with powdered activated carbon 23. In this way, during the heating and reduction process, the hydrogen gas used for the reduction can substantially fully envelop the rods 11. The carbon 23 is provided (in powdered, solid or granular form) for removing excess moisture from the interior space 5 during the heating and reduction process. The inventors have found that without the carbon 23, there is a greater risk of over reduction which affects the formation of the desired Magneli phases. Over time, the absorption of water vapour results in the carbon 23 being consumed as it is converted into carbon dioxide. The activated carbon 23 must, therefore, be replenished or replaced from time to time. In the preferred embodiment, the carbon is replaced every three production cycles.
The four frames 9 are positioned side by side in two rows and two columns and the outer sides of the frames 9 (ie the sides closest to the heating elements 7) are clad in a protective shielding 25, such as a ceramic fibre or a low thermal mass insulation blanket, to minimise (if not avoid) the exposure of the rods 11 to direct radiant heat from the heating elements 7. In the preferred embodiment, the protective shielding 25 is standard grade Fiberfrax® Durablanket® of 96 kg/m3 density and 25 mm thick, which is made of blown alumino-silicate ceramic fibre and classified to operate at temperatures of 125O0C. The shielding 25 is attached to the frames 9 and hangs down below the bottom of the rods 11. A gap 26 of approximately 25mm is provided between the bottom of the shielding 25 and the tray 21 to allow for good circulation of the hydrogen gas during the heating and reduction process.
An oxygen meter (not shown) and two thermocouples (not shown) are located at different positions in the interior space 5 and are provided for generating measurements to aid in the control of the manufacturing process.
A description has been given above of the kiln assembly 1 used in this embodiment. A description will now be given of the way in which the kiln assembly 1 is used to manufacture Ebonex® rods 11 in this embodiment.
Production Process Figure 3 is a flowchart illustrating the production process used in this embodiment. As shown, in step Sl, the kiln assembly 1 is prepared, by suspending the rods 11 of titanium oxide from the frames 9; adding activated carbon 23; sealing the internal space 5 by lowering the hood 3 into the oil-filled trough 8; opening the inlet 10 and the outlet 12 and closing the top vent 14. Once the hood 3 is in place, nitrogen is pumped into the inlet 10, in step S3, at a rate of approximately three cubic meters per hour for a minimum of fifty minutes, in order to purge the interior space 5 of oxygen. An oxygen meter (not shown) is used to confirm when the oxygen has been removed to the 2% level. At this point, the nitrogen flow is stopped and, in step S5, hydrogen is pumped into the inlet 10 at a rate of approximately four cubic meters per hour. Hydrogen will continue to be pumped into the inlet 10 until the end of the heating and reduction process and throughout the subsequent cooling. After about 50 minutes have elapsed from the start of the hydrogen introduction, the oxygen meter is again consulted to ensure the remaining oxygen level is below 2% before a further oxygen test is undertaken. This test includes filling a small container with gas from the outlet 12 and, at a safe distance, applying a lit taper to the container. If the gas held within the container ignites with a loud pop, then this indicates that the oxygen level in the interior space 5 remains too high to proceed with the reduction process. Whereas, if the gas held within the container burns slowly, with a lazy flame, then it is safe to proceed with the reduction process. The hydrogen escaping at the outlet 12 is then lit and allowed to burn off as the reduction process proceeds.
The heating process is then started, in step S7, by switching on the heating elements 7. The initial heating is controlled in steps S9 and Sl 1 by a controller so that the interior space 5 is heated at a rate not exceeding 200 0C /hour. Once the internal temperature reaches the operating temperature of between 1170 0C and 1190 0C (controlled in steps S13 and S 14), the controller maintains the operating temperature in step S15 for approximately 5.5 hours. At the end of this time the heating elements 7 are switched off and the kiln 1 is allowed to cool naturally in step S 16 until the internal temperature is below 200 0C (which typically takes about fourteen hours). Figure 4 shows the typical temperature variation inside the kiln 1 during the production process and illustrating the initial heating stage, the reduction stage and the cooling stage.
The inventors have found that there is no detriment to the rods 11 if they remain in the kiln 1 for longer periods (after the heating elements 7 have been switched off), but they found that removing them earlier can result in crazing which affects their quality. Once the internal temperature is below 200 °C (as determined in step S 17), the hydrogen flow is halted, the outlet 12 is closed and the top vent 14 is opened. Nitrogen gas is then pumped in via the inlet 10 into the internal space 5 to purge the hydrogen gas out via the top vent 14 where it is lit and allowed to burn off. Once the flame has extinguished, indicating that there is no more hydrogen within the interior space 5, the hood 3 is removed in step S19 and the rods 11 are removed and tested in step S20. In this embodiment in step S20, each rod 11 is tested using the following semi- empirical tests:
1. By a colour observation (by a human or machine). Magneli phases have a characteristic blue-black colouration, and this is required to be uniform over the length of the rod 11 ; any discolouration is taken as evidence of unwanted oxides having been formed.
2. A two-point probe electrical conductivity test, in which a current of 100 mA is passed through the rod 11 and the voltage drop measured between two probes on the rod 11 that are a placed 100 mm apart from each other is compared with a threshold and if it is greater then the rod fails.
Failure of either or both tests results in the rod being rejected.
In addition to the above tests, X-ray diffraction measurements may be obtained on some or all of the rods 11 to confirm the Magneli phases that are present.
The inventors have found that holding the rods 11 freely within the interior space 5 results in better quality Ebonex® rods 11 being produced in a more consistent manner with fewer breakages compared to the prior art method described above. The inventors also found that rods 11 processed in the above manner have a significantly greater conductivity compared to the rods 11 obtained using the prior art process discussed above. In particular, the inventors have found that typically rods 11 obtained using the above process and when tested using the above test, exhibit lower average voltage drops, indicating higher conductivities, than rods obtained using the prior art process. Table 1 below, illustrates the typical spread of measured voltage drops in millivolts achieved in one production run across ten arbitrary positions across the top plate 13 using the above described production method. Table 1
Figure imgf000010_0001
As shown, the average voltage drop is about 35 millivolts. In contrast, similar tests performed on rods manufactured using the prior art technique, results in typical measured voltage drops in the range of 65 to 70 millivolts, with some as high as 120 to 130 millivolts. In the latter case, those rods would then be reprocessed by running them through the heating and reduction process again.
Modifications and Alternatives
In the above embodiment, the precursor rods were hung from a frame within the kiln. In an alternative embodiment the rods may be stood directly on the floor of the kiln 1, but the inventors found that this resulted in a greater percentage of the rods being broken during the heating and reduction process, hi a further alternative, the precursors may be supported by one or more supports so that they can be fully enveloped by the reducing gas. In the above embodiment, precursor tubular rods were heated in the kiln to produce Ebonex® tubular rods. As those skilled in the art will appreciate, other shaped precursors can be used. For example, the precursors can be plates, tiles, sheets etc. Additionally, the resulting Ebonex® material may be pulverised to produce Ebonex® powder.
In the above embodiment the rods were fully enveloped in the reducing gas during the reduction process. As those skilled in the art will appreciate it would be possible to cover a portion of each rod (for example, one end of each rod) and still produce the rods using the present invention. The term "fully enveloped" used in the description and the claims should therefore be construed broadly to also cover the situation where the rods are substantially fully enveloped.
In the above embodiment, a controller was used to control the heating and reduction process. As those skilled in the art will appreciate, this controller can be a human controller or an automated one.

Claims

Claims:
1. A method of manufacturing substoichiometric oxides of titanium, the method comprising: placing a titanium oxide precursor into the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space to heat the precursor and the reducing gas to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium; characterised in that said placing step places said precursor in said interior space so that said reducing gas can substantially fully envelop said precursor.
2. A method according to claim I3 wherein said heating step uses a plurality of heating elements located within the interior space of said kiln.
3. A method according to claim 2, further comprising shielding said precursor from radiant heat produced by said heating elements.
4. A method according to claim 3, wherein said shielding step uses a thermal insulator to shield said precursor.
5. A method according to claim 4, comprising holding said precursor by a support and providing said thermal insulator between the support and the heating elements.
6. A method according to claim 5, comprising providing said thermal insulator between said support and said heating elements to leave a gap between a lower edge of the thermal insulator and a base of the kiln, to thereby allow free circulation of said reducing gas around said precursor.
7. A method according to any preceding claim, wherein said placing step places a plurality of said precursors within said interior space of the kiln so that said plurality of precursors are reduced during said heating step.
8. A method according to any preceding claim, wherein said heating step includes an initial heating stage in which the interior space is heated at a rate not exceeding a predetermined threshold until the interior space is above a predetermined operating temperature.
9. A method according to claim 8, wherein said initial heating stage heats the interior space at a rate not exceeding 200 0C per hour.
10. A method according to claim 8 or 9, wherein said initial heating stage ends when said interior space reaches an operating temperature above 1170 0C.
11. A method according to any of claims 8 to 10, wherein said heating step includes a second heating stage in which the temperature of the interior space is held within a predetermined operating temperature range for a predetermined period of time.
12. A method according to claim 11, wherein said second heating stage maintains the temperature of the interior space within a temperature range between 1170 0C and 1190 0C for said predetermined period of time.
13. A method according to claim 11 or 12, wherein said second heating stage maintains said interior space within said operating temperature range for a period of time of between five and eight hours.
14. A method according to any preceding claim, comprising stopping said heating step and allowing said interior space to cool down to a predetermined temperature.
15. A method according to claim 14, comprising removing the precursor from the kiln after the interior space has cooled down below 200 0C.
16. A method according to any preceding claim, wherein said introducing step introduces said reducing gas at a predetermined rate during said heating step.
17. A method according to claim 16, wherein said introducing step introduces said reducing gas at a rate of between two and five cubic meters per hour.
18. A method according to any preceding claim, comprising suspending said precursor from a support within said interior space so that said precursor is held freely within said interior space.
19. A method according to any preceding claim, comprising testing said precursor after said heating step to determine if the desired substoichiometric titanium oxides have been formed and rejecting the precursor if it is determined that the desired substoichiometric titanium oxides have not been formed.
20. A method according to claim 19, wherein said testing step includes visually inspecting the precursor to observe the colouration thereof.
21. A method according to claim 19 or 20, wherein said testing step includes determining a measure of the conductivity of the precursor after the heating step and comparing the determined measure with a predefined threshold value.
22. A method according to any preceding claim, comprising providing a desiccant within the interior space of the kiln to absorb moisture generated during the heating step.
23. A method according to claim 22, wherein said desiccant comprises powdered activated carbon.
24. A method according to any preceding claim, wherein said precursor is rod shaped or a plate shaped.
25. A method according to claim 24, further comprising pulverising the precursor after said heating step to form powdered substoichiometric oxides of titanium.
26. An apparatus for manufacturing substoichiometric oxides of titanium, the apparatus comprising: a kiln having a base and a hood defining an interior space of the kiln; a support operable to hold a titanium oxide precursor in the interior space of the kiln; an inlet for introducing a reducing gas into the interior space of the kiln; and heating elements operable to heat the interior space of the kiln to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium; characterised in that said support is operable to hold said precursor in said interior space so that said reducing gas can substantially fully envelop said precursor.
27. An apparatus according to claim 26, wherein said heating elements are located within the interior space of said kiln.
28. An apparatus according to claim 27, further comprising shielding material for shielding said precursor from radiant heat produced by said heating elements.
29. An apparatus according to claim 28, wherein said shielding material comprises a thermal insulator to shield said precursor.
30. An apparatus according to claim 29, wherein said thermal insulator is provided between the support and the heating elements.
31. An apparatus according to claim 30, wherein said thermal insulator is positioned between said support and said heating elements so that a gap is provided between a lower edge of the thermal insulator and a base of the kiln, to thereby facilitate free circulation of said reducing gas around said precursor.
32. An apparatus according to any of claims 26 to 31, wherein said support is operable to hold a plurality of said precursors within said interior space of the kiln so that said plurality of precursors can be reduced at the same time.
33. An apparatus according to any of claims 26 to 32, comprising a controller operable to control said heating elements so that, during an initial heating stage, the interior space is heated at a rate not exceeding a predetermined threshold until the interior space is above a predetermined operating temperature.
34. An apparatus according to claim 33, wherein said controller is operable to control said heating elements so that, during said initial heating stage, the interior space is heated at a rate not exceeding 200 0C per hour.
35. An apparatus according to claim 33 or 34, wherein said controller is operable to control said heating elements so that said initial heating stage ends when said interior space reaches an operating temperature above 1170 0C.
36. An apparatus according to any of claims 33 to 35, wherein said controller is operable to control said heating elements so that, during a second heating stage, the temperature of the interior space is held within a predetermined operating temperature range for a predetermined period of time .
37. An apparatus according to claim 36, wherein said controller is operable to control said heating elements so that said second heating stage maintains the temperature of the interior space within a temperature range between 1170 0C and 11900C for said predetermined period of time.
38. An apparatus according to claim 36 or 37, wherein said controller is operable to control said heating elements so that said second heating stage maintains said interior space within said operating temperature range for a period of time of between five and eight hours.
39. An apparatus according to any of claims 33 to 38, wherein said controller is operable to switch off said heating elements to allow said interior space to cool down to a predetermined temperature.
40. An apparatus according to claim 39, comprising means for removing the precursor from the kiln after the interior space has cooled down below 200 0C.
41. An apparatus according to any of claims 26 to 40, comprising a controller operable to control the rate at which said reducing gas is introduced into said interior space.
42. An apparatus according to claim 41, wherein said controller is operable to control said inlet so that said reducing gas is introduced at a rate of between two and five cubic meters per hour.
43. An apparatus according to any of claims 26 to 42, wherein said support is operable to suspend said precursor so that said precursor is held freely within said interior space.
44. An apparatus according to any of claims 26 to 43, further comprising means for testing said precursor after said heating step to determine if the desired substoichiometric titanium oxides have been formed and means for rejecting the precursor if it is determined that the desired substoichiometric titanium oxides have not been formed.
45. An apparatus according to claim 44, wherein said testing means includes means for visually inspecting the precursor to observe the colouration thereof.
46. An apparatus according to claim 44 or 45, wherein said testing means includes means for determining a measure of the conductivity of the precursor after the heating step and means for comparing the determined measure with a predefined threshold value.
47. An apparatus according to any of claims 26 to 46, further comprising a tray for holding a desiccant within the interior space of the kiln to absorb moisture generated during the reduction process.
48. An apparatus according to claim 47, wherein said desiccant comprises powdered activated carbon.
49. An apparatus according to any of claims 26 to 48, wherein said precursor is rod shaped or plate shaped.
50. An apparatus according to claim 49, further comprising means for pulverising the precursor after said heating step to form powdered substoichiometric oxides of titanium.
51. A method of manufacturing substoichiometric oxides of titanium, the method comprising: placing a titanium oxide precursor into the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space to heat the precursor and the reducing gas to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium; characterised in that said placing step places said precursor in said interior space so that the majority of the heating of the precursor performed in said heating step is achieved by convection.
52. A method of manufacturing substoichiometric oxides of titanium, the method comprising: holding a titanium oxide precursor in the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space to heat the precursor and the reducing gas to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium; characterised in that said holding step holds said precursor in said interior space so that said reducing gas can flow freely, substantially over the entire surface of said precursor.
53. A method of manufacturing substoichiometric oxides of titanium, the method comprising: placing a titanium oxide precursor into the interior space of a kiln; introducing a reducing gas into the interior space; and heating the interior space to heat the precursor and the reducing gas to cause the reduction of the titanium oxide precursor to form the substoichiometric oxides of titanium; characterised in that said heating step includes an initial heating stage in which the interior space of the kiln is heated at a rate not exceeding a predetermined threshold until the temperature of the interior space reaches an operating temperature range.
54. An article comprising substoichiometric oxides of titanium, the article being manufactured using the method of any of claims 1 to 25, 51, 52 or 53.
PCT/GB2006/003573 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen WO2008037941A1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US12/443,091 US20100040533A1 (en) 2006-09-26 2006-09-26 Method of producing substoichiometric oxides of titanium by reduction with hydrogen
JP2009529748A JP2010504903A (en) 2006-09-26 2006-09-26 Process for producing substoichiometric titanium oxide by hydrogen reduction
CN200680056210A CN101547863A (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen
AU2006348872A AU2006348872A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen
CA002664733A CA2664733A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen
EP06794576A EP2066587A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen
PCT/GB2006/003573 WO2008037941A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen
IL197840A IL197840A0 (en) 2006-09-26 2009-03-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/GB2006/003573 WO2008037941A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen

Publications (1)

Publication Number Publication Date
WO2008037941A1 true WO2008037941A1 (en) 2008-04-03

Family

ID=37532982

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2006/003573 WO2008037941A1 (en) 2006-09-26 2006-09-26 A method of producing substoichiometric oxides of titanium by reduction with hydrogen

Country Status (8)

Country Link
US (1) US20100040533A1 (en)
EP (1) EP2066587A1 (en)
JP (1) JP2010504903A (en)
CN (1) CN101547863A (en)
AU (1) AU2006348872A1 (en)
CA (1) CA2664733A1 (en)
IL (1) IL197840A0 (en)
WO (1) WO2008037941A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009024776A1 (en) * 2007-08-23 2009-02-26 Atraverda Limited Powders

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9672953B2 (en) 2014-03-27 2017-06-06 EboNEXT Technologies (BVI) Devices and methods for advanced phase-locked materials
CN111514875A (en) * 2020-05-06 2020-08-11 青岛理工大学 Three-dimensional electrode based on titanium tetroxide catalytic particles and application thereof in sewage treatment
CN115557532B (en) * 2022-07-12 2024-01-26 沈阳工程学院 Preparation method and device of titanium tetraoxide micro powder

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0047595A1 (en) * 1980-09-10 1982-03-17 Marston Palmer Ltd. Electrochemical cell
WO1992014683A1 (en) * 1991-02-21 1992-09-03 Atraverda Ltd. Conductive titanium suboxide particulates
US6168426B1 (en) * 1996-02-19 2001-01-02 Murata Manufacturing Co., Ltd. Batch-type kiln

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2029648A (en) * 1933-09-28 1936-02-04 Oliver V Austin Fertilizer production from sewage
US4166147A (en) * 1973-04-16 1979-08-28 Minnesota Mining And Manufacturing Company Shaped and fired articles of tio2
US4912286A (en) * 1988-08-16 1990-03-27 Ebonex Technologies Inc. Electrical conductors formed of sub-oxides of titanium
JPH03221779A (en) * 1990-01-25 1991-09-30 Murata Mfg Co Ltd Heat treating furnace
GB9021053D0 (en) * 1990-09-27 1990-11-07 Ici Plc Production of reduced titanium oxide
JP3233055B2 (en) * 1996-02-19 2001-11-26 株式会社村田製作所 Batch type heat treatment furnace
JP2006100683A (en) * 2004-09-30 2006-04-13 Sumitomo Chemical Co Ltd Thermoelectric conversion material for titanium oxide
US7513061B2 (en) * 2006-05-26 2009-04-07 Dai-Ichi High Frequency Co., Ltd. Sludge dehydrating processor for converting sludge including organic substance into resources of low water content

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0047595A1 (en) * 1980-09-10 1982-03-17 Marston Palmer Ltd. Electrochemical cell
WO1992014683A1 (en) * 1991-02-21 1992-09-03 Atraverda Ltd. Conductive titanium suboxide particulates
US5281496A (en) * 1991-02-21 1994-01-25 Atraverda Limited Electrochemical cell containing a titanium suboxide electrode
US6168426B1 (en) * 1996-02-19 2001-01-02 Murata Manufacturing Co., Ltd. Batch-type kiln

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009024776A1 (en) * 2007-08-23 2009-02-26 Atraverda Limited Powders
US8377342B2 (en) 2007-08-23 2013-02-19 Atraverda Limited Titanium suboxide powders

Also Published As

Publication number Publication date
CN101547863A (en) 2009-09-30
IL197840A0 (en) 2009-12-24
EP2066587A1 (en) 2009-06-10
AU2006348872A2 (en) 2009-06-25
JP2010504903A (en) 2010-02-18
US20100040533A1 (en) 2010-02-18
AU2006348872A1 (en) 2008-04-03
CA2664733A1 (en) 2008-04-03

Similar Documents

Publication Publication Date Title
KR101310437B1 (en) Heater, apparatus, and associated method
JP4565159B2 (en) Temperature fixed point cell, temperature fixed point device, and thermometer calibration method
US20100040533A1 (en) Method of producing substoichiometric oxides of titanium by reduction with hydrogen
CN213813437U (en) Aluminum electrolysis cell simulation test device and aluminum electrolysis cell simulation test system
CN104674344A (en) Growth device, growth furnace and preparation method of yttrium lithium fluoride laser crystals
EP2640872A2 (en) Electrolysis apparatus
GB2442229A (en) Method and apparatus for the manufacture of substoichiometric oxides of titanium
CN102589964B (en) Heating device
Edler et al. Comparison of nickel–carbon and iron–carbon eutectic fixed point cells for the calibration of thermocouples
CN109269935A (en) A kind of insulation cover and the method using filter paper ashing time in its shortening gravimetry
CN112595762A (en) Aluminum electrolysis cell simulation test device and aluminum electrolysis cell simulation test system
US5749932A (en) Refractory electrodes for joule heating and methods of using same
US20210008613A1 (en) Method and Preparing a Charge Ingot for Producing Articles by Casting
JPH04300239A (en) Method for sintering ceramic product
CN111929342A (en) Test system and method for evaluating physical properties of viscous layer of hot surface of blast furnace hearth
CN113219121B (en) Oxidation simulation experiment device and method
Caruso et al. Experimental comparison of cathode rodding practices
RU221301U1 (en) Heating device for capillaries made of molybdenum glass, sealed and filled with alkali metal
CN113406137B (en) Method for testing solid-liquid phase line temperature of steel sample
Simakov et al. Tests for resistance to cryolite: methods and comparative evaluation
Richards Thermal Expansion of Uranium and Tantalum Monocarbides up to 2700 C
CN212566857U (en) High-temperature tube furnace for graphene preparation
da Silva et al. Understanding immersion in zinc fixed-point cells using factorial design of experiments
BR0300960B1 (en) system to graphite carbon bodies.
CN110669922B (en) Device and method for aerobic roasting of oxidized pellets

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200680056210.6

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 06794576

Country of ref document: EP

Kind code of ref document: A1

ENP Entry into the national phase

Ref document number: 2009529748

Country of ref document: JP

Kind code of ref document: A

ENP Entry into the national phase

Ref document number: 2664733

Country of ref document: CA

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2006794576

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2246/DELNP/2009

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2006348872

Country of ref document: AU

ENP Entry into the national phase

Ref document number: 2006348872

Country of ref document: AU

Date of ref document: 20060926

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 12443091

Country of ref document: US